CATIA复合材料结构设计课件.ppt
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1、CATIA复合材料结构设计,Copyright DASSAULT SYSTEMES,1,Copyright DASSAULT SYSTEMES,2,Course Presentation,Objectives of the courseIn this course you will learn how to generate Composites parts for aerospace from Preliminary Design to Manufacturing Detail DesignTargeted audienceComposites for Aerospace DesignerP
2、rerequisitesPart DesignAssembly Design Wireframe and Surface DesignDrafting,4 days,Copyright DASSAULT SYSTEMES,3,Planning(1/2),Copyright DASSAULT SYSTEMES,4,Planning(2/2),Copyright DASSAULT SYSTEMES,5,Table of Contents(1/8),PRELIMINARY DESIGNCPD Workbench Presentation p.13Accessing the Workbench p.1
3、4General presentation p.15CPD Preliminary Design tools p.16CPD Engineering Detail Design toolsp.17CPD Manufacturing Detail Design toolsp.18Composites Catalogp.20Defining New Material p.21Defining FEA Properties p.22Defining Composites Parametersp.23Laminate Parameters p.24Selectioning Material Catal
4、og p.25Defining Directions p.26Group of Zones p.27Creating Group of Zones p.28,Copyright DASSAULT SYSTEMES,6,Table of Contents(2/8),Zones Parametersp.29Creating Zone contours p.30Creating Laminate p.31Selecting Rosette p.32Modifying Zone contoursp.33Modifying Laminatep.34Transition Zonesp.35Defining
5、 Transition Zone p.36Modifying Transition Zonep.37Refining Transition Zonep.38Connection Generator p.39Analyzing Structural Zonesp.40Analyzing Transition Zonesp.41Storing/Checking the Connection Generator Featurep.42Updating the Connection Generator Featurep.43Impose Thickness Point p.44Defining an
6、ITPp.45Modifying an ITP p.46,Copyright DASSAULT SYSTEMES,7,Table of Contents(3/8),Stack-up file from Zones p.47Creating an Excel Stack-Up File p.48Zone Connections optionp.49Modifying Stack-Up Filep.50Import Laminatep.55Importing Laminatep.56Solid and Top Surface from Zones p.57Defining Solidp.58Def
7、ining Top Surfacep.59Plies Creation From Zonesp.60Creating Plies From Zones with Tapers p.61Creating Plies From Zones with Staggering valuep.62,Copyright DASSAULT SYSTEMES,8,Table of Contents(4/8),ENGINEERING DETAILED DESIGNLimit Contourp.65Relimiting Plies Geometry p.66Limit contour on Plies from Z
8、ones with Staggering Value p.67Plies Groupp.69Creating Plies Group Automaticallyp.70Creating Plies Group Manually p.71Manual Plies Creation p.72Defining Geometry p.73Defining Attributes p.74Core p.75Defining Core p.76Modifying Core p.77Ply Exploder p.78Exploding Plies into Surfaces p.79Cross-Section
9、ing with DMU p.80,Copyright DASSAULT SYSTEMES,9,Table of Contents(5/8),Managing the Part p.83Reordering the Partp.84Replacing Shellp.85Renaming a Zonep.86Renaming a Taperp.89Ply shadingp.92Removing Ply Shellsp.93Symmetry Creation p.94Defining a Symmetry Pivotp.95Defining a Symmetry Non Pivotp.96Ply
10、Table p.97Creating a Complete Excel Ply Table Filep.98Creating an Excel Ply Table File per Group of Pliesp.99Numerical Analysisp.100Defining Numerical Analysisp.101Exporting Numerical Analysisp.102,Copyright DASSAULT SYSTEMES,10,Table of Contents(6/8),Core Sample p.103Core Sampling Analysisp.104Core
11、 Sampling Storagep.105Core Sampling Exportp.106Drawing p.107Drawing Generationp.108Defining General Sheet:Solid activep.109Defining General Sheet:Explode activep.111Defining Sheet for Table Integrationp.115,Copyright DASSAULT SYSTEMES,11,Table of Contents(7/8),MANUFACTURING DETAILED DESIGNManufactur
12、ing Data Structure p.118 Defining Manufacturing Data Structurep.119Manufacturing Surface Swapping p.120Swapping Manufacturing Surfacep.121Edge Of Partp.123Creating Engineering Edge Of Part(EEOP)p.124Creating Manufacturing Edge Of Part(MEOP)p.125Material Excess p.126Defining Material Excessp.127Multi
13、 Splice Creation p.128Defining a Multi Splicep.129 Producibility Analysisp.132Defining Producibility Analysisp.133Storing Producibility Analysisp.134,Copyright DASSAULT SYSTEMES,12,Table of Contents(8/8),Darts p.135Defining dartsp.136Flattening p.138Defining Flatten with Rotated optionp.139Defining
14、Flatten without Rotated optionp.140Export p.141Exporting Plies:2D and 3D entitiesp.142,Copyright DASSAULT SYSTEMES,13,CPD Workbench Presentation,You will become familiar with Aerospace Composites Preliminary Design main featuresAccessing the WorkbenchGeneral presentationCPD Preliminary Design toolsC
15、PD Engineering Detail Design toolsCPD Manufacturing Detail Design tools,Copyright DASSAULT SYSTEMES,14,Accessing the Workbench,Accessing the WorkbenchModifying CATIA environmentTools/Option/GeneralGeneralUser Interface Style:CATIA P3,Copyright DASSAULT SYSTEMES,15,General presentation,CPD tools,CPD
16、features,Product tree,Standard tools,Copyright DASSAULT SYSTEMES,16,Parameters,Creating Zones:Contours+Laminate,Creating Transition Zone,ITP Creation,Connection Generator,Plies Creation From Zone,Zones Group,Stack-up file from Zones,Solid and Top Surface from Zones Creation,Import Laminate,CPD Preli
17、minary Design tools,Copyright DASSAULT SYSTEMES,17,Core Sample,Core Definition,Stacking Order Modification,Stack-up file from Plies,Group of Plies Definition,Numerical Analysis,Manual Plies:Definition/Modification,CPD Engineering Detail Design tools,Ply Exploder,Symmetry Pivot/Non Pivot,Copyright DA
18、SSAULT SYSTEMES,18,IGES/DXF Export,Material Excess,EOP Definition,Producibility Analysis,Create Manufacturing Data,Flatten,Manufacturing Skin Swapping,CPD Manufacturing Detail Design tools,Limit Contour,Multi Splice,Copyright DASSAULT SYSTEMES,19,Composites Preliminary Design Product,Preliminary Des
19、ign Tools,Copyright DASSAULT SYSTEMES,20,Composites Catalog,You will become familiar with Defining the Composites CatalogDefining New materialDefining FEA propertiesDefining Composites parameters,Copyright DASSAULT SYSTEMES,21,Defining New Material,1-Click Insert the menu toolbar,2-Select New Materi
20、al option,5-Indicate the New material name,4-Select the Feature Properties option,3-Double click on New Material option,Copyright DASSAULT SYSTEMES,22,Defining FEA Properties,7-Select the Type of material,8-Indicate FEA properties values,5-Select the Analysis option,6-Select the Material option,Copy
21、right DASSAULT SYSTEMES,23,Defining Composites Parameters,9-Select the Composites option,10-Indicate Composites parameters values,11-Press OK for validation,Copyright DASSAULT SYSTEMES,24,Laminate Parameters,You will become familiar with Defining the Laminate ParametersSelectioning Material CatalogD
22、efining Plies Direction,Copyright DASSAULT SYSTEMES,25,Selectioning Material Catalog,1-Click the Parameters icon,2-Select the Material Catalog tab,3-Select the Material Catalog,4-Click Open for selection,Copyright DASSAULT SYSTEMES,26,Defining Directions,5-Create New Direction,8-Click OK for validat
23、ion,6-Reorder Directions,7-Remove the Unused Directions,Copyright DASSAULT SYSTEMES,27,Group of Zones,You will become familiar with Defining the Group of ZonesCreating Group of Zones,Copyright DASSAULT SYSTEMES,28,Creating Group of Zones,1-Click the Zones Group icon,2-Select the Shell Support,3-Sele
24、ct the Draping direction,5-Click OK for validation,4-Select the Rosette,Copyright DASSAULT SYSTEMES,29,Zones parameters,You will become familiar with defining the zone parametersCreating Zone contoursCreating LaminateSelecting RosetteModifying Zone contoursModifying Laminate,Copyright DASSAULT SYSTE
25、MES,30,Creating Zone Contours,1,2,3,4,1-Click the Zone icon,2-Click the Geometry tab,3-Select the Zones Group,4-Select the curves which define the zone contour:Respect a logical order,(1 to 4)or(4 to 1),Copyright DASSAULT SYSTEMES,31,Creating Laminate,8-Indicate the Number of plies per orientation a
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